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机译:Numerical study of high temperature non-equilibrium effects of double-wedge in hypervelocity flow
School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China;
College of Aerospace Engineering, Chongqing University, Chongqing 400044, China;
State Key Laboratory of High-Temperature Gas Dynamics, Institute of Mechanics, CAS, Beijing 100190, China;
Hypervelocity double-wedge flow; High temperature non-equilibrium effects; Laminar and turbulence flow; Shock wave interaction; Shock wave/boundary layer interaction;